Flight test of an active vibration control system on the UH-60 black hawk helicopter

Annual Forum Proceedings - American Helicopter Society

Volumn 1, Issue , 1995, Pages 393-402

  Welsh, W ^a   Fredrickson, C ^a   Rauch, C ^a   Lyndon, I ^a  

^a UNITED TECHNOLOGIES CORPORATION   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

ADAPTIVE CONTROL SYSTEMS; FLIGHT DYNAMICS; FUSELAGES; HELICOPTER ROTORS; ROBUSTNESS (CONTROL SYSTEMS); VIBRATION CONTROL; VIBRATION MEASUREMENT;

ACTIVE VIBRATION CONTROL SYSTEM; FLIGHT TEST; SERVO INERTIAL FORCE GENERATORS; VIBRATORY LOADS;

MILITARY HELICOPTERS;

EID: 0029455393     PISSN: 07334249     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)